KIT NO: 02216
F-7II is an aircraft developed from the F-7I. The maiden flight was on December 30,1978. Primary modifications included: self-designed ejection seats and equipment instead of those formerly designed by Russia, a backward opening canopy with fixed front windproof windows, and a modified Pen-7engine which solved the problem of height temperature in the rear fuselage. The landing parachute is located at the end of vertical tail with enlarged fuel tanks.
